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Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction

Alexander Steinwandel, Walter Fichter, Institute of Flightmechanics, Control

May 5, 2015

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Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction

  • Presented at Forum 71
  • 9 pages
  • SKU # : 71-2015-056
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Effects of 2/rev Trailing Edge Flap Input on Helicopter Vibrations for Concurrent Vibration and Noise Reduction

Authors / Details: Alexander Steinwandel and Walter Fichter, Institute of Flightmechanics and Control

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